How to Calculate Pressure Ratio for High Mach Number?
Pressure Ratio for High Mach Number calculator uses Pressure Ratio = (Mach Number ahead of shock/Mach Number behind shock)^(2*Specific Heat Ratio/(Specific Heat Ratio-1)) to calculate the Pressure Ratio, The Pressure ratio for high Mach number formula is defined as the ratio of Mach number before and after the shock raise to the power of specific heat ratio. Pressure Ratio is denoted by rp symbol.
How to calculate Pressure Ratio for High Mach Number using this online calculator? To use this online calculator for Pressure Ratio for High Mach Number, enter Mach Number ahead of shock (M1), Mach Number behind shock (M2) & Specific Heat Ratio (Y) and hit the calculate button. Here is how the Pressure Ratio for High Mach Number calculation can be explained with given input values -> 350.4666 = (1.5/0.5)^(2*1.6/(1.6-1)).